DIAMANT DEB
NORAD 2685
Debris
LEO
1967-014F
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LEO · NORAD 2685
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
520 km
Apogee
1006 km
Inclination
38.9°
Period
100.1 min
Mean Motion
14.38637647 rev/day
TLE Epoch
2026-09-18 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude763 km
Orbital Velocity26,909 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.39
Eccentricity0.0341
Semi-Major Axis7,134 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1967-02-15
Launch Site
Hammaguir, Algeria
Int'l Designator
1967-014F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIAMANT DEB is a tracked piece of space debris attributed to France, launched on 1967-02-15 from Hammaguir, Algeria on the Diademe D-1D launch. After more than 59 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 520 km and 1,006 km with an inclination of 38.9°. It travels at approximately 26,909 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.39 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, DIAMANT DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
DIAMANT DEB orbits at an average altitude of 763 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of DIAMANT DEB’s average altitude, there are currently 425 active payloads and 2,231 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0455. With an inclination of 38.9°, DIAMANT DEB passes over latitudes between 38.9°N and 38.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. France operates approximately 124 active satellites in total, of which 4 share a similar altitude band with DIAMANT DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
DIAMANT DEB orbits in Low Earth Orbit (LEO) at altitudes between 520 km (perigee) and 1,006 km (apogee), with an average altitude of approximately 763 km. It completes one orbit every 100 minutes, travelling at approximately 26,909 km/h (16,721 mph).
DIAMANT DEB (NORAD ID 2685) is a piece of tracked orbital debris attributed to France. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
DIAMANT DEB was launched on 1967-02-15 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAMANT DEB (NORAD ID 2685) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
DIAMANT DEB travels at approximately 26,909 km/h (16,721 mph) — roughly 7.47 km/s. It completes 14.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.47 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like DIAMANT DEB. Read more about debris statistics and the Kessler syndrome.